AD 2016-17-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aviat | Various | Airworthiness Directives; RUAG Aerospace Services GmbH Airplanes |
Unsafe Condition
Excessive wear on the guide pin of the power lever or condition lever, which could cause functional loss of the flight idle stop.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the guide pins of the power levers and condition levers. Replace any pin that exceeds allowable wear limits. Perform repetitive detailed inspections based on specified compliance times.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 9,600 flight hours or 9,600 flight cycles, whichever occurs first.
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Affected Aircraft
RUAG Aerospace Services GmbH Models 228-100, 228-101, 228-200, 228-201, 228-202, and 228-212 airplanes, all serial numbers, certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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